49.025.05 黑色金属合金综合 标准查询与下载

BS EN 4575:2020 航空航天系列 耐热合金X12CrNiCoMoW21-20 溶液经过处理和除垢 板材和板材 3毫米

BS EN 4573:2020 航空航天系列 耐热合金X12CrNiCoMoW21-20 固溶处理和沉淀处理 棒材和型材 深度≤100毫米

What is BS EN 4573 about?    BS EN 4573 discusses standards for heat-resisting alloy, solution-treated, and precipitation-treated bars, and sections for aerospace applications. BS EN 4573 is part of the series of European metallic material standards for aerospace applications. BS EN 4573 specifies the requirements relating to:   Heat-resisting alloy X12CrNiCoMoW21-20   Solution treated and precipitation treated

Aerospace series. Heat resisting alloy X12CrNiCoMoW21-20. Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm

BS EN 4572:2020 航空航天系列 耐热合金 X12CrNiCoMoW21-20 固溶处理 板材和带材 a≤3毫米

What is BS EN 4572 about?    BS EN 4572 discusses standards for heat-resisting alloy, solution-treated, sheets and strips for aerospace applications. BS EN 4572 is part of the series of European metallic material standards for aerospace applications. BS EN 4572 specifies the requirements relating to:   Heat-resisting alloy X12CrNiCoMoW21-20  

Aerospace series. Heat resisting alloy X12CrNiCoMoW21- 20. Solution treated. Sheets and strips. a ≤ 3 mm

BS EN 4574:2020 航空航天系列 耐热合金X12CrNiCoMoW21-20 固溶处理和沉淀处理 锻件 深度≤100毫米

What is BS EN 4574 about?    BS EN 4574 discusses standards for heat-resisting alloy, solution-treated, precipitation-treated forgings, for aerospace applications. BS EN 4574 is part of the series of European metallic material standards for aerospace applications.   BS EN 4574 specifies the requirements relating to:   Heat-resisting alloy X12CrNiCoMoW21-20  

Aerospace series. Heat resisting alloy X12CrNiCoMoW21- 20. Solution treated and precipitation treated. Forgings. De ≤ 100 mm

BS EN 4571:2020 航空航天系列 耐热合金 X12CrNiCoMoW21-20 固溶处理 棒材和型材 深度≤100毫米

What is BS EN 4571 about?    BS EN 4571 discusses standards for heat-resisting alloy, solution-treated bars, and sections for aerospace applications. BS EN 4571 is part of the series of European metallic material standards for aerospace applications. BS EN 4571 specifies the requirements relating to:   Heat-resisting alloy X12CrNiCoMoW21-20  

Aerospace series. Heat resisting alloy X12CrNiCoMoW21- 20. Solution treated. Bars and sections. De ≤ 100 mm

BS EN 3761:2020 航空航天系列 耐热合金FE-PA2601 软化并冷加工 锻造紧固件棒材 D≤50毫米 1 100 MPa ≤ Rm ≤ 1 300 MPa

What is BS EN 3761 about?    BS EN 3761 is a part of the series of European metallic material standards for aerospace applications. BS EN 3761 specifies the following requirements for aerospace applications:   Heat resisting alloy FE-PA2601   Softened and cold worked   Bar for forged fasteners

Aerospace series. Heat resisting alloy FE-PA2601. Softened and cold worked. Bar for forged fasteners. D ≤ 50 mm. 1 100 MPa ≤ Rm ≤ 1 300 MPa

BS EN 3510:2019 航空航天系列 耐热合金 FE-PA2602 (X4NiCrTiMoV26-15) 固溶处理和沉淀处理 棒材和型材 深度≤100毫米

What is BS EN 3510- Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) bars and sections for aerospace applications about?   BS EN 3510 is a metallic material standard that covers technical specifications for heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) bars and sections for aerospace applications, enhancing the thermal resistance that increases the performance and longevity of aerospace structures and parts.   BS EN 3510 specifies the requirements for heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) bars and sections in the solution treated and precipitation treated delivery condition. BS EN 3510 sets a limit dimension range of De ≤ 100 mm for aerospace applications.   Who is BS EN 3510- Heat...

Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Bars and sections. De ≤ 100 mm

BS EN 2119:2017 航空航天系列. 耐热合金FE - PA2601(X6NiCrTiMoV26-15). 溶液处理和沉淀处理. 铆钉用线材. 2毫米D10毫米960兆帕

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated. Wires for rivets. 2 mm D 10 mm. Rm 960 MPa

DIN EN 2119:2018 航空航天系列. 耐热合金FE - PA2601 (X6NiCrTiMoV26-15). 固溶处理和沉淀处理-铆钉用线材- 2mm≤D≤10 mm - Rm≥960 MPa ：德文和英文版本EN 2119:2017

This European Standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated Wires for rivets 2 mm

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets -2 mm <= D <= 10 mm - Rm >= 960 MPa; German and English version EN 2119:2017

EN 2119:2017 航空航天系列 耐热合金 FE-PA2601（X6NiCrTiMoV26-15） 固溶处理和沉淀处理 铆钉用钢丝 2 mm ～D ～10 mm Rm ～960 MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm ��D ��10 mm - Rm ��960 MPa

BS EN 6072:2010 航空航天系列.金属材料.试验方法.横幅疲劳试验

This European Standard defines a method to determine constant amplitude fatigue data of metallic materials and the S-N curve (or Wöhler curve).

Aerospace series. Metallic materials. Test methods. Constant amplitude fatigue testing

DS/EN 6072:2010 航空航天系列 金属材料 试验方法 等幅疲劳试验

This European Standard defines a method to determine constant amplitude fatigue data of metallic materials and the S N curve (or Wöhler curve).

Aerospace series - Metallic materials - Test methods - Constant amplitude fatigue testing

SAE AMS2175A-2010 铸件的分类和检验

This specification establishes nondestructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castings. This specification has been used typically for structural castings, but usage is not limited to such applications.

Castings, Classification and Inspection of

EN 6072:2010 航空航天系列.金属材料.试验方法.横幅疲劳试验

This European Standard defines a method to determine constant amplitude fatigue data of metallic materials and the S-N curve (or W？hler curve).

Aerospace series - Metallic materials - Test methods - Constant amplitude fatigue testing

SAE AMS5916A-2009 35Fe 24Cr 37Ni 0.65Cb 0.2N退火的耐腐蚀和耐高温合金薄板材、带材和厚板材

This specification covers a corrosion and heat resistant alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring corrosion and oxidation resistance up to 1800 °F (982 °C), and relatively high strength up to 1500 °F (816 °C), but usage is not limited to such applications.

Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 35Fe 24Cr 37Ni 0.65Cb 0.2N Annealed

SAE AIR4129-2008 金属晶须

This AIR presents an abbreviated review of the metallurgical phenomena known as whiskers. It is not all encompassing, but rather it is intended to introduce the design engineer to the technical issues of metallic whiskers and the problems they can cause.

Metallic Whiskers

BS EN 4314:2007 航空航天系列.FE-PA2602(X4NiCrTiMoV26-15)型耐热合金.非热处理的锻坯a/D≤250mm

This standard specifies the requirements relating to: Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) — Non heat treated, forging stock a or D ≤ 250 mm for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 250 mm

BS EN 4317:2007 航空航天系列.FE-PA2601(X6NiCrTiMoV26-15)型耐热合金.非热处理的锻坯.a/D≤200mm

This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) — Non heat treated, forging stock a or D ≤ 200 mm for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm

DIN EN 4315:2008 航空航天系列.FE-PA2601 (X6NiCrTiMoV26-15)型耐热合金.溶解处理和沉淀处理的棒材和型材.a或D≤100mm、Rm≥900MPa

This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) -- Solution treated and precipitation treated, bar and section a or D ≤100 mm, Rm ≥ 900 MPa for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D 100 mm, R_m 900 MPa; German and English version EN 4315:2007

DIN EN 4317:2008 航空航天系列.耐热合金 FE-PA2601 (X6NiCrTiMoV26-15).非热处理的锻件.a/D≤200 mm

This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)- Non heat treated, forging stock a or D ≤200 mm for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D 200 mm; German and English version EN 4317:2007